US12024282B2 - Guidance device, flying object, air defense system and guidance program - Google Patents
Guidance device, flying object, air defense system and guidance program Download PDFInfo
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- US12024282B2 US12024282B2 US17/087,955 US202017087955A US12024282B2 US 12024282 B2 US12024282 B2 US 12024282B2 US 202017087955 A US202017087955 A US 202017087955A US 12024282 B2 US12024282 B2 US 12024282B2
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- flying object
- flying
- processing device
- patrol
- control
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- 230000007123 defense Effects 0.000 title claims description 68
- 238000004891 communication Methods 0.000 claims abstract description 21
- 238000004146 energy storage Methods 0.000 claims description 24
- 238000001514 detection method Methods 0.000 claims description 18
- 238000000034 method Methods 0.000 description 56
- 238000010586 diagram Methods 0.000 description 12
- 239000002360 explosive Substances 0.000 description 12
- 239000000446 fuel Substances 0.000 description 6
- 238000004590 computer program Methods 0.000 description 4
- 239000003380 propellant Substances 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 239000002828 fuel tank Substances 0.000 description 2
- 230000002401 inhibitory effect Effects 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 239000003721 gunpowder Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/15—Propulsion using combustion exhausts other than turbojets or turbofans, e.g. using rockets, ramjets, scramjets or pulse-reactors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
- G05D1/102—Simultaneous control of position or course in three dimensions specially adapted for aircraft specially adapted for vertical take-off of aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/12—Target-seeking control
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/60—Intended control result
- G05D1/656—Interaction with payloads or external entities
- G05D1/686—Maintaining a relative position with respect to moving targets, e.g. following animals or humans
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/15—UAVs specially adapted for particular uses or applications for conventional or electronic warfare
- B64U2101/18—UAVs specially adapted for particular uses or applications for conventional or electronic warfare for dropping bombs; for firing ammunition
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Definitions
- the processing device ( 124 ) of one of other flying objects ( 100 ) generates, based on the notification signal, a deployment control signal to control the propulsion device ( 110 ) of the one of other flying objects ( 100 ) so that the one of other flying objects ( 100 ) flies toward the first patrol path from a second patrol path.
- FIG. 1 It is a schematic diagram of an air defense system according to an embodiment.
- FIG. 6 A It is a flowchart that shows processes of an interception module according to an embodiment.
- FIG. 11 It is a configuration diagram of a storage device according to an embodiment.
- a propulsion device 110 is provided with a rotary wing 111 , a motor 112 and a rocket engine 113 .
- the motor 112 rotates the rotary wing 111 to make the flying object 100 fly.
- the rocket engine 113 injects a propellant such as compressed air to give thrust to the flying object 100 .
- the rocket engine 113 is used when flying toward the target at high speed, when rapidly changing a direction of travel, or the like.
- a plurality of rocket engines 113 are provided so as to be able to inject the propellant in four directions: front, rear, left and right, for example. By selectively start rocket engines 113 , the flying object 100 can fly toward the target 20 .
- a plurality of rocket engines 113 may be provided so as to be able to inject the propellant in up-and-down directions.
- the propulsion devices 110 are not limited to the above as long as they can give thrust to the flying object 100 and control the direction of travel.
- the propulsion device 110 may be provided with a jet engine.
- the energy container 150 supplies energy to the propulsion device 110 .
- the energy container 150 stores electric power to rotate motor 112 and fuel of rocket engine 113 .
- the energy container 150 may measure an energy storage quantity of the electric power and the fuel that are stored.
- the energy container 150 includes a fuel tank, a battery, or the like.
- the guidance device 120 controls the propulsion device 110 , the detection device 130 and the explosive device 140 .
- the guidance device 120 may be, as shown in FIG. 3 , provided with a communication device 121 , an input and output device 122 , a memory device 123 and a processing device 124 .
- the communication device 121 is electrically connected to the propulsion device 110 , the detection device 130 , the explosive device 140 and the energy container 150 and perform communication with respective devices by wire or wirelessly.
- the communication device 121 performs communication with external devices such as other flying objects 100 .
- the communication device 121 transfers data received from respective devices to the processing device 124 .
- the communication device 121 transfers signals generated by the processing device 124 to respective devices.
- the communication device 121 includes various interfaces such as Network Interface Card (NIC) and Universal Serial Bus (USB).
- NIC Network Interface Card
- USB Universal Serial Bus
- the input and output device 122 receives information for the processing device 124 to execute processes. In addition, the input and output device 122 outputs a result of processes executed by the processing device 124 .
- the input and output device 122 includes a variety of input devices and output devices, and includes for example a keyboard, a mouse, a microphone, a display, a speaker, a touch panel, or the like. The input and output device 122 may be removed when no information is inputted.
- the memory device 123 stores various data for guiding the flying objects 100 , such as a guidance program 200 .
- the memory device 123 is used as a non-transitory tangible storage medium that stores the guidance program 200 .
- the guidance program 200 may be provided as a computer program product stored in a recording medium 50 readable by a computer or may be provided as a computer program product downloadable from a server.
- the guidance program 200 executed by the processing device 124 is provided with a patrol module 210 , an interception module 220 and a deployment module 230 .
- the processing devices 124 (for example, the processing device 124 of the flying object 100 - 1 ) generates a patrol control signal to control the propulsion device 110 (for example, the propulsion device 110 of the flying object 100 - 1 ) so as to fly along a patrol path set on the defense line 30 .
- the processing device 124 controls the propulsion device 110 (for example, the propulsion device 110 of the flying object 100 - 1 ) so that the flying object 100 (for example, the flying object 100 - 1 ) performs a hovering at the position indicated by the patrol path.
- the processing device 124 (for example, the processing device 124 of the flying object 100 - 1 ) generates an interception control signal to control the propulsion device 110 (for example, the propulsion device 110 of the flying object 100 - 1 ) so that the flying object 100 (for example, the flying object 100 - 1 ) flies toward the target 20 .
- the processing device 124 (for example, the processing device 124 of the flying object 100 - 1 ) may, when the flying object 100 (for example, the flying object 100 - 1 ) reaches a vicinity of the target 20 , detonate the explosive device 140 .
- the processing device 124 uses a thrust generated by the rotary wing 111 to make the flying object 100 (for example, the flying object 100 - 1 ) fly toward the target 20 .
- the processing device 124 (for example, the processing device 124 of the flying object 100 - 1 ) may use a rocket engine 113 to make the flying object 100 (for example, the flying object 100 - 1 ) fly toward the target 20 .
- the processing device 124 may control the propulsion device 110 (for example, the propulsion device 110 of the flying object 100 - 2 ) so as to fly toward a first patrol path where another flying object 100 (for example, the flying object 100 - 1 ) was flying.
- the processing device 124 (for example, the processing device 124 of the flying object 100 - 2 ) may make the flying object 100 (for example, the flying object 100 - 2 ) fly toward a predetermined patrol path.
- the flying objects 100 are deployed on the defense line 30 so as to surround the protection target 10 .
- the flying objects 100 fly to deployment positions that are predetermined on the defense line 30 .
- the flying objects 100 may automatically fly to the deployment positions under control of the guidance device 120 or may fly to the deployment positions by remote control.
- the processing device 124 determines in step S 110 whether information of the target 20 is received.
- the detection device 130 transmits, when detecting the target 20 , information of the target 20 to the processing device 124 via the communication device 121 .
- the processing device 124 executes, when the information of the target 20 is received (step S 110 : Yes), a process in step S 120 in order to determine whether to intercept the target 20 .
- the processing device 124 executes a process in step S 150 .
- step S 130 the processing device 124 determines whether the calculated threat level of the target 20 is equal to or higher than a desired threshold value. When the threat level is equal to or higher than the desired threshold value, the processing device 124 moves to a process in step S 140 to intercept the target 20 and executes the interception module 220 . The processing device 124 transmits, when executing the interception module 220 , a notification signal that indicates a departure from the patrol path to other flying objects 100 . When the threat level is less than the desired threshold value, the processing device 124 executes a process in step S 150 .
- the processing device 124 transmits, when executing the interception module 220 , a notification signal that indicates a departure from the patrol path to other flying objects 100 . In case of not intercepting the target 20 (step S 160 : No), the processing device 124 executes a process in step S 170 shown in FIG. 5 B .
- the patrol module 210 can make the flying object 100 fly along a desired patrol path.
- the flying objects 100 can rapidly deal with the target 20 by flying from the defense line 30 to the target 20 .
- the flying objects 100 can wait for the interception on the target 20 until the target 20 reaches a vicinity of the defense line 30 and the air defense system 1000 can efficiently deal with the target 20 .
- the air defense system 1000 can deal with a plurality of targets 20 since a plurality of flying objects 100 patrol on the defense line 30 .
- step S 230 the processing device 124 determines whether a distance from the own flying object to the target 20 is equal to or shorter than a first distance.
- the first distance includes a distance in that the explosive device 140 can destroy surrounding moving objects by exploding.
- the processing device 124 detonates the explosive device 140 in step S 240 . By detonating the explosive device 140 , the target 20 is destroyed.
- the processing device 124 executes a process in step S 250 .
- step S 250 the processing device 124 determines whether the distance from the own flying object to the target 20 is equal to or shorter than a second distance.
- the second distance includes a distance that the rocket engine 113 can fly.
- step S 250 : Yes the processing device 124 executes a process in step S 260 .
- step S 250 : No the processing device 124 executes a process in step S 270 shown in FIG. 6 B .
- step S 260 shown in FIG. 6 A the processing device 124 starts the rocket engine 113 .
- the flying object 100 can fly at high speed toward the target 20 and rapidly change the direction of travel.
- the processing device 124 may determine, when the target 20 does not exist in the direction the flying object 100 travels for example, that the flying object 100 cannot intercept the target 20 . This is because it indicates that the flying object 100 has passed the target 20 . In addition, the processing device 124 may determine, in a case a distance from the own flying object to the target 20 is measured and this distance does not shorten after a flight, that the target 20 cannot be intercepted.
- the deployment module 230 is executed when another flying object 100 flies toward the target in order to change a patrol path of the own flying object.
- the deployment module 230 makes the processing device 124 execute processes shown in FIG. 7 .
- step S 340 the processing device 124 determines whether the own flying object is to intercept the target 20 that could not be intercepted. For example, the processing device 124 calculates, when flying toward the target 20 , a predicted intercept point where the target 20 is reached. The processing device 124 determines a priority level based on a distance from the own flying object to the predicted intercept point. When the priority level is equal to or higher than a desired threshold value, the processing device 124 determines that the target 20 is to intercept. The processing device 124 moves, when intercepting the target 20 (step S 340 : Yes), to a process in step S 350 to execute the interception module 220 . In case of not intercepting the target 20 (step S 340 : No), the processing device 124 executes a process in step S 360 shown in FIG. 7 .
- step S 360 the processing device 124 determines whether the position indicated by the patrol path to change is reached.
- the processing device 124 compares a position of the own flying object and the position indicated by the patrol path to change. When a distance from the position of the own flying object to the position indicated by the patrol path is shorter than a desired threshold value, the processing device 124 determines that the position indicated by the patrol path is reached.
- the processing device 124 executes in step S 370 the patrol module 210 . While the flying object 100 does not reach the position indicated by the patrol path (step S 360 : No), the processing device 124 returns to the process of step S 320 and repeats the process.
- the flying objects 100 can fly toward the patrol path and the air defense system 1000 can be efficiently deployed.
- a flying object 100 can protect the protection target 10 in collaboration with other flying objects 100 .
- the storage device 300 is provided with a hangar 310 , an energy supply device 320 and a central control device 330 .
- the hangar 310 stores a plurality of flying objects 100 .
- the hangar 310 may have a plurality of hangar spaces each of that stores a flying object 100 .
- the hangar spaces may be divided by a wall from each other.
- the central control device 330 may be provided with a communication device 331 , an input and output device 332 , a memory device 333 and a processing device 334 .
- the communication device 331 is electrically connected to the flying objects 100 , the hangar 310 and the energy supply device 320 , and performs communication with respective devices by wire or wirelessly.
- the communication device 331 transfers data received from respective devices to the processing device 334 .
- the communication device 331 transfers signals generated by the processing device 334 to respective devices.
- the communication device 331 includes various interfaces such as NIC or USB.
- the input and output device 332 receives information for the processing device 334 to execute processes. In addition, the input and output device 332 outputs a result of processes executed by the processing device 334 . For example, information of the defense line 30 is inputted to the input and output device 332 . In addition, information of the flying objects 100 such as positions, remaining energy quantity may be outputted to the input and output device 332 .
- the input and output device 332 includes a variety of input devices and output devices, and includes for example a keyboard, a mouse, a microphone, a display, a speaker, a touch panel and the like. The input and output device 332 may be removed when no information is inputted.
- the storage device 300 supplies, when a flying object 100 is stored in the hangar 310 , energy to the flying object 100 by the energy supply device 320 .
- the hangar 310 is provided with a sensor that detects that a flying object 100 is stored.
- the energy supply device 320 acquires a remaining energy quantity from the flying object 100 and supplies energy to the flying object 100 based on the remaining energy quantity.
- the storage device 300 can make the flying objects 100 fly toward the defense line 30 .
- the flying objects 100 can fly toward the defense line 30 based on a notification signal transmitted by another flying object 100 .
- the central control device 330 may be provided separately from the storage device 300 .
- a flying object 100 may automatically return to the storage device 300 when the energy storage quantity is less than a return limit quantity.
- the guidance program 200 B is provided with the patrol module 210 , the interception module 220 , the deployment module 230 and a return module 240 .
- the configuration except the guidance program 200 B is similar to the first and second embodiments and therefore detailed description will be omitted.
- the patrol module 210 , the interception module 220 and the deployment module 230 are similar to the first and second embodiments and therefore detailed description will be omitted.
- the processing device 124 controls the flying object 100 so as to return based on the energy storage quantity by executing the return module 240 .
- the return module 240 makes the processing device 124 execute processes shown in FIG. 16 .
- the patrol path may be determined in accordance with a number of the flying objects 100 in patrol on the defense line 30 .
- the patrol path may be set so that the flying objects 100 fly equidistantly on the defense line 30 .
- the guidance device 120 determines the patrol path in accordance with the number of the flying objects 100 on the defense line 30 .
- the guidance device 120 updates the number of the flying objects 100 in patrol by storing a number of flying objects 100 that have flown from the storage device 300 toward the defense line 30 and receiving notification signals.
- the processing device 124 of the guidance device 120 generates a patrol start signal indicating that the patrol path is reached and transmits it to other flying objects 100 .
- the other flying objects 100 updates the number of the flying objects 100 in patrol and change the patrol paths.
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- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Traffic Control Systems (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Description
Claims (8)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2019230926A JP7413003B2 (en) | 2019-12-20 | 2019-12-20 | Guidance equipment, air vehicles, air defense systems, and guidance programs |
| JP2019-230926 | 2019-12-20 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20210188431A1 US20210188431A1 (en) | 2021-06-24 |
| US12024282B2 true US12024282B2 (en) | 2024-07-02 |
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| Application Number | Title | Priority Date | Filing Date |
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| US17/087,955 Active 2041-12-07 US12024282B2 (en) | 2019-12-20 | 2020-11-03 | Guidance device, flying object, air defense system and guidance program |
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| Country | Link |
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| US (1) | US12024282B2 (en) |
| JP (1) | JP7413003B2 (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11879705B2 (en) * | 2018-07-05 | 2024-01-23 | Mikael Bror Taveniku | System and method for active shooter defense |
| US20230280768A1 (en) * | 2022-03-01 | 2023-09-07 | Rockwell Collins, Inc. | Primary asset escort through threatened airspace by an autonomous aerial vehicle team |
| CN115388719B (en) * | 2022-08-24 | 2024-01-16 | 天津津航计算技术研究所 | Aircraft laser irradiation route planning method based on laser guided weapon |
| CN118088390B (en) * | 2024-01-19 | 2025-08-08 | 星逻智能科技(苏州)有限公司 | Fan inspection method and device, storage medium and electronic equipment |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2017174110A (en) | 2016-03-23 | 2017-09-28 | 株式会社Jvcケンウッド | Unmanned mobile device, takeover method, program |
| US20180251218A1 (en) | 2015-09-16 | 2018-09-06 | Christopher Wilkinson | Space Combat Drone |
| US20180341262A1 (en) * | 2017-05-29 | 2018-11-29 | Plasan Sasa Ltd. | Drone-Based Active Protection System |
| US20190025858A1 (en) * | 2016-10-09 | 2019-01-24 | Airspace Systems, Inc. | Flight control using computer vision |
| US20190063881A1 (en) | 2017-08-25 | 2019-02-28 | Aurora Flight Sciences Corporation | Aerial Vehicle Interception System |
| US20190114929A1 (en) | 2017-10-12 | 2019-04-18 | Topcon Corporation | Data processing device, drone, and control device, method, and processing program therefor |
| US20190285388A1 (en) * | 2018-03-13 | 2019-09-19 | Elta Systems Ltd. | Drone interceptor system, and methods and computer program products useful in conjunction therewith |
| US20200064443A1 (en) * | 2018-08-21 | 2020-02-27 | Sung Wook Yoon | Method of identifying and neutralizing low-altitude unmanned aerial vehicle |
| US20200108924A1 (en) * | 2018-10-03 | 2020-04-09 | Sarcos Corp. | Close Proximity Countermeasures for Neutralizing Target Aerial Vehicles |
| US20200108926A1 (en) * | 2018-10-03 | 2020-04-09 | Sarcos Corp. | Aerial Vehicles Having Countermeasures Deployed From a Platform for Neutralizing Target Aerial Vehicles |
| US20200269978A1 (en) * | 2018-08-24 | 2020-08-27 | Hangzhou Zero Zero Technology Co., Ltd. | Detachable protection structure for unmanned aerial systems |
| US20210309364A1 (en) * | 2018-12-17 | 2021-10-07 | Autel Robotics Co., Ltd. | Automatic return method, appratus and unmanned aerial vehicle |
-
2019
- 2019-12-20 JP JP2019230926A patent/JP7413003B2/en active Active
-
2020
- 2020-11-03 US US17/087,955 patent/US12024282B2/en active Active
Patent Citations (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20180251218A1 (en) | 2015-09-16 | 2018-09-06 | Christopher Wilkinson | Space Combat Drone |
| JP2017174110A (en) | 2016-03-23 | 2017-09-28 | 株式会社Jvcケンウッド | Unmanned mobile device, takeover method, program |
| US20190019051A1 (en) | 2016-03-23 | 2019-01-17 | JVC Kenwood Corporation | Unmanned mobile apparatus capable of transferring imaging, method of transferring |
| US20190025858A1 (en) * | 2016-10-09 | 2019-01-24 | Airspace Systems, Inc. | Flight control using computer vision |
| US20180341262A1 (en) * | 2017-05-29 | 2018-11-29 | Plasan Sasa Ltd. | Drone-Based Active Protection System |
| JP2019023553A (en) | 2017-05-29 | 2019-02-14 | プラサン・ササ・リミテッド | Drone type active protection system |
| JP2019060589A (en) | 2017-08-25 | 2019-04-18 | オーロラ フライト サイエンシズ コーポレーション | Aerial vehicle interception system |
| US20190063881A1 (en) | 2017-08-25 | 2019-02-28 | Aurora Flight Sciences Corporation | Aerial Vehicle Interception System |
| US20200041234A1 (en) * | 2017-08-25 | 2020-02-06 | Aurora Flight Sciences Corporation | Aerial Vehicle Interception System |
| US20190114929A1 (en) | 2017-10-12 | 2019-04-18 | Topcon Corporation | Data processing device, drone, and control device, method, and processing program therefor |
| JP2019073056A (en) | 2017-10-12 | 2019-05-16 | 株式会社トプコン | Unmanned aircraft control device, unmanned aircraft, data processing device, unmanned aircraft control method and program for control of unmanned aircraft |
| US20190285388A1 (en) * | 2018-03-13 | 2019-09-19 | Elta Systems Ltd. | Drone interceptor system, and methods and computer program products useful in conjunction therewith |
| US20200064443A1 (en) * | 2018-08-21 | 2020-02-27 | Sung Wook Yoon | Method of identifying and neutralizing low-altitude unmanned aerial vehicle |
| US20200269978A1 (en) * | 2018-08-24 | 2020-08-27 | Hangzhou Zero Zero Technology Co., Ltd. | Detachable protection structure for unmanned aerial systems |
| US20200108924A1 (en) * | 2018-10-03 | 2020-04-09 | Sarcos Corp. | Close Proximity Countermeasures for Neutralizing Target Aerial Vehicles |
| US20200108926A1 (en) * | 2018-10-03 | 2020-04-09 | Sarcos Corp. | Aerial Vehicles Having Countermeasures Deployed From a Platform for Neutralizing Target Aerial Vehicles |
| US20210309364A1 (en) * | 2018-12-17 | 2021-10-07 | Autel Robotics Co., Ltd. | Automatic return method, appratus and unmanned aerial vehicle |
Non-Patent Citations (1)
| Title |
|---|
| Office Action issued Aug. 1, 2023 in Japanese Patent Application No. 2019-230926, with English translation, 11 pages. |
Also Published As
| Publication number | Publication date |
|---|---|
| US20210188431A1 (en) | 2021-06-24 |
| JP7413003B2 (en) | 2024-01-15 |
| JP2021099181A (en) | 2021-07-01 |
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